DocumentCode :
1683092
Title :
Low cost attitude determination system for a LEO information mini-satellite
Author :
Somov, Yevgeny ; Butyrin, Sergey ; Somov, Sergey ; Hajiyev, Chingiz
Author_Institution :
Samara State Tech. Univ., Samara, Russia
fYear :
2015
Firstpage :
725
Lastpage :
730
Abstract :
We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite´s orbital motion.
Keywords :
artificial satellites; calibration; inertial navigation; satellite navigation; signal processing; space vehicle navigation; LEO information mini-satellite; SINS calibration; SINS correction; in-flight signal processing; low Earth orbit; low cost attitude determination system; mini-satellite orbital motion long-term forecasting; strap-down inertial navigation system; sun-magnetic system; Calibration; Estimation; Magnetometers; Mathematical model; Measurement uncertainty; Position measurement; Quaternions; SINS; calibration; mini-satellite; signal processing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2015 7th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4673-7760-7
Type :
conf
DOI :
10.1109/RAST.2015.7208436
Filename :
7208436
Link To Document :
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